On-Line Trajectory Retargeting for Alternate Landing Sites

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,961.00
Award Year:
2004
Program:
SBIR
Phase:
Phase I
Contract:
NNM04AA53C
Award Id:
67314
Agency Tracking Number:
034642
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
1160 Pepsi Place, Suite 300, Charlottesville, VA, 22901
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
120839477
Principal Investigator:
John Schierman
Principal Investigator
(434) 973-1215
schierman@barron-associates.com
Business Contact:
David Ward
Business Official
(434) 973-1215
barron@barron-associates.com
Research Institute:
n/a
Abstract
Barron Associates, Inc. proposes to develop a novel on-line trajectory optimization approach for Reusable Launch Vehicles (RLVs) under failure scenarios, targeting alternative abort-landing sites. Key features of the proposed approach are: An innovative on-line optimization approach: By describing decision variables (variables whose optimal solutions are sought) in terms of appropriate basis functions, the trajectory optimization problem can be reformulated to find the relatively few basis function coefficients that characterize the desired trajectory. This significantly reduces the search domain, enabling rapid convergence to feasible solutions. This key idea will be coupled with a numerical optimization approach known as Piecewise Linear Programming (PLP), which has been used successfully in related programs requiring on-line, real-time optimal solu-tions. A generic bootstrapping capability: To improve the speed and robustness of the on-line procedure, a method will be developed to generate initializing trajectories for the on-line optimization that are suitable for all recoverable ranges, vehicle configurations, energy conditions, and abort scenarios. Phase I simulation studies will demonstrate on-line generation of alternative re-entry trajectories for dif-ferent landing targets and vehicle configurations. Computation time and accuracy will be assessed from the simulation studies.

* information listed above is at the time of submission.

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